DIGITAL TWIN OF A HIGH-ENERGY SYSTEM USING ALUMINUM HYDRIDE AS A FUEL

Numerical modeling of the fl ow of combustion products of the propellant containing an aluminum hydride admixture in the nozzle of a solid-propellant rocket engine has been carried out. The advantage of aluminum hydride over aluminum when used in composite solid propellants has been shown.
   
Author:  A. B. Vorozhtsov and N. N. D′yachenko
Keywords:  two-phase fl ow, polydisperse ensemble of particles, specifi c momentum
Page:  972